N119HQ
Registered owner: REPUBLIC AIRWAYS INC, IN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
AFT SERVICE DOOR OPEN MSG IN FLIGHT. R2 DOOR SHOWED AS OPEN ON STATUS PAGE FOR APPROX 10 MINUTES - NO CHANGE IN PRESSURIZATION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. FOUND R2 DOOR LATCH SENSOR TO BE OUT OF ADJUSTMENT. ADJUSTED R2 DOOR LATCH SENSOR.
EXTERNAL SKIN DOUBLER REPAIR IS MISSING THE CUTOUT FILLERS REQUIRED BY ETD2019-170-098492 REV. B.TECHNICIAN REPAIRED AAI DISCREPANCY ITEM #5: REPUBLIC REPAIR #39 - FR 20-21 S17L--18L - EXTERNAL SKIN DOUBLER REPAIR IS MISSING THE CUTOUT FILLERS REQUIRED BY ETD2019-170-098492 REV. B PART B
RH COCKPIT FLOOR DOUBLER IS CORRODED AT SEVERAL LOCATIONS FROM FR 8 TO FR 12 AS MARKED.TECHNICIAN REPAIRED R/H COCKPIT FLOOR DOUBLER BETWEEN FR 8- FR12 IAW 53-10-10 REPAIR 07
CORROSION - RT INBD SEAT TRACK AT FR15.REPAIRED RT INBD SEAT TRACK AT FR15 IAW SRM 53-10-10 /REPAIR 01P
CORROSION - LT INBD SEAT TRACK AT FR18.MECHANIC PERFORMED CUTOUT AT LH I/B SEAT TRACK AT FR18 IAW REF. SRIIM CH. 51, REF. EMB SRM 53-10-10 /REPAIR 01P
RH I/B SEAT TRACK HAS 3 CORRODED RIVETS ON I/B FLANGE AT FR59.TECHNICIAN REPAIRED RH I/B SEAT TRACK SECTION BETWEEN FR56 AND FR60 .REF. EMB SRM 53-00-10 REPAIR 01
AVNX MAU 1A FAIL IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED NIC PROC 1 MODULE.
FWD EMERGENCY LIGHT BATTERY FAILED FUNC TEST. R&R FWD LH EMERGENCY LIGHT BATTERY.
HORIZONTAL STABILIZER FAILED ROLL BACK LASH CHECK. REPAIRED HORIZONTAL STABILIZER STABILIZER FITTINGS REF EMB ETD2024-170-007213. BACKLASH CHECK GOOD.
CORROSION ON CFIII SKIN DOUBLER BETWEEN FRAME 76 AND 77 STRINGER 28R AND 29R. PERFORMED CUTOUT OF INTERNAL DOUBLER BETWEEN FRAMES 76-77 STGR 28R-29R. INSTALLED INTERNAL FILLER AND EXTERNAL SKIN DOUBLER ON CFIII BETWEEN FRAMES 76-77 AND STGRS 28R AND 29R REFER ETD-2024-170-007454.
DURING CLEANING - CORROSION ALONG STRINGER ROW 29R , BETWEEN FRAME 76 TO FRAME 77. PERFORMED PERMANENT REPAIR BY SPLICE REPAIR ON STGR 29R SPLICE REPAIR FR 75-76 TO FR 78-79 IN ACCORDANCE WITH, REF ETD2024-170-007444-A.
DURING THE REMOVAL OF FWD CARGO LOWER THRESHOLD BEAM. THE FWD FINGER DOUBLER WAS FOUND GOUGE. REMOVED AND REPLACED FWD FINGER DOUBLER ON FWD CARGO DOOR. REF SRM 51-40-08.
FWD. CARGO DOOR CUTOUT, LOWER BEAM CORRODED AT AFT LATCH FITTING AS MARKED. REMOVE AND REPLACE FWD CARGO LOWER THRESHOLD BEAM BETWEEN FRAMES 24-27 REFER SRM 51-40-08.
CORRODED SHEAR CLIP FRAME 88, STRINGER 28R. REMOVED CORRODED SHEAR CLIP FRAME 88, STRINGER 28R LOCATED AND DRILLED NEW SHEAR CLIP PN 170-66531-001 REF EMB SRM 51-40-08, 51-40-02. INSTALLED SHEAR CLIP FRAME 88, STRINGER 28R TRANSFERRED FROM H9447 SN 652 REF EMB SRM 51-40-08. INSTALLATION OF THIS SHEAR CLIP HAS BEEN TRANSFERRED TO H9447 SERIAL NUMBER:00386
WASTE SERVICE DOOR CUTOUT DOUBLER CORRODED ON FWD SIDE. REMOVED AND REPLACED WASTE SERVICE DOOR CUTOUT INTERNAL DOUBLER REFER SRM 51-40-08. RESTORED SURFACE PROTECTION TO REWORKED AREA REFER SRM 51-23-06, CPM 51-25-00.
L1 DOOR HARD TO OPEN. C/W FIM TASK 52-11-00-810-806-A, FOUND WEAK COUNTERBALANCE RODS AND L1 DOOR BOX MECHANISM LACKING LUBRICATION. R & R COUNTERBALANCE RODS AND LUBED L1 DOOR BOX MECHANISM.
PHOTOLUMINESCENT FLOOR STRIP AT SEAT ROW 10DF TO 12DF. R & R PHOTOLUMINESCENT FLOOR STRIP.
L1 OUTSIDE DOOR HANDLE JAMMED. REMOVED FOD FROM L1 DOOR. PERFORMED OPERATIONAL CHECK IAW AMM 52-11-00. OPS CHECK GOOD.
MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED L1 DOOR.
GATE AGENT HAD TROUBLE OPENING L1 DOOR. CLEANED AND LUBRICATED L1 DOOR COMMAND RAMPS IAW 53-10-21.
COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE - REMOVED AND REPLACED FWD RH EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01, OPS CHECK GOOD. COCKPIT EMERGENCY LIGHT OPS CHECK GOOD
WHILE IN HEAVY CHECK - RIGHT HAND SHEAR PANEL FR87 - FR88 HAS CORROSION. REMOVE AND REPLACED RT SHEAR PANEL P/N 170-91919-001 REF SRM 51-40-08.
DURING HEAVY CHECK - WHILE PERFORMING 2195:170EO-53-14-0002-170EO-53-14-0002 L1 DOOR LOWER BEAM REWORK FOUND CORROSION AROUND FWD AND AFT GIRT BAR FITTINGS AS MARKED. REPLACED BEAM.
WHILE IN HEAVY CHECK - LT GUSSET PANEL FR. 90 HAS CORROSION AS MARKED. REPLACED GUSSET WITH NEW AND TOP-COATED, REF. SRM 51-40-08 AND 51-23-06.
WHILE IN HEAVY CHECK - CENTER SPLICE FR 90 HAS CORROSION AS MARKED. INSTALLED NEW SPLICE AT FR90 AND APPLIED TOPCOAT. REF. SRM (51-40-08) (51-23-06)
WHILE IN HEAVY CHECK - LEFT HAND UPPER SHEET 2" FWD FR 85 - FR 86 HAS CORROSION AS MARKED. INSTALLED NEW SHEET (P/N: 170-86101-001) AT LT FR85-86 AND APPLIED TOPCOAT TO FASTENERS REF. SRM (51-40-08) (51-23-06)
WHILE IN HEAVY CHECK - RIGHT HAND UPPER SHEET 2" FORWARD FR 85-FR86 HAS CORROSION AS MARKED. INSTALLED NEW RT SHEET (P/N:170-86101-001) AT FR85-86 AND APPLIED TOPCOAT REF. SRM (51-40-08) (51-23-06)
WHILE IN HEAVY CHECK - RIGHT HAND PANEL SUPPORT FR 87 - FR 90 HAS CORROSION AS MARKED. REPLACED RT PANEL SUPPORT AT FR87-90 REF. SRM (51-40-08)
WHILE IN HEAVY CHECK - CENTER SHEAR PANEL FR87 - FR88 HAS CORROSION. REPLACED CORRODED CENTER SHEAR PANEL FROM FR87-88. REF. SRM (51-40-08)
WHILE IN HEAVY CHECK - RT HORIZONTAL STAB RIB 12A FOUND TO BE CRACKED. REMOVED AND REPLACED RIB 12A ON RT HORIZONTAL STABILIZER BETWEEN FRONT AND MID-SPAR REF SRM 51-40-08.
WHILE IN HEAVY CHECK - RT HORIZONTAL STAB RIB 11 CRACKED AFT OF FWD SPAR. REMOVED AND REPLACED RIB NR 11 FOR THE RT HORIZONTAL STABILIZER BETWEEN FRONT AND MID-SPARS REF. SRM 51-40-08.
DURING HEAVY CHECK - LH HORIZONTAL STAB RIB 11 CRACKED AFT OF FWD SPAR. REMOVED AND REPLACED RIB 11A ON LT HORIZONTAL STAB,
WHILE IN HEAVY CHECK - CORROSION-STRINGER 19L AROUND FASTENERS BETWEEN FR82-FR83. REMOVED AND INSTALLED NEW LT SHEAR PANEL AND SHEAR PANEL SPLICE REF SRM 51-40-08.
MAIN CABIN DOOR WILL NOT CLOSE. SEQUENCED THE DOOR IAW AMM 52-10-00. OPS CHECKED GOOD.
L2 DOOR HANDLE NOT ARMING. FOUND PLASTIC COVER (SITE GLASS) TO BUSTLE BINDING THE DOOR ASSY. REMOVED ALL PARTS, L2 OPERATING NORMALLY. NO FURTHER DEFECTS FOUND IAW CMM 52-12-22.
FWD RT SILL HAS TWO SPOTS OF CORROSION ONE FWD OF FR 13 AND ONE AT FR 14 INBD SIDE AS MARKED. AIRCRAFT REMAINS IN HEAVY CHECK BNA.
CORROSION FOUND ON FWD WARDROBE SUPPORT BETWEEN FRAMES 17 AND 18 REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-04 AND 51-242-01
CORROSION IN STRINGER 19R FR 89-90. PERFORMED SPLICE REPAIR PER ETD2016-170-114325.
CORROSION IN STR21R BETWEEN FR 89-90. REMOVED AND REPLACED STRINGER AND SPLICE AT STR 21R FR89 TO 90 REF SRM 51-41-01, 51-41-02 AND 51-43-03.
CORROSION IN RT SHEAR PANEL BETWEEN FR 87-88. REMOVED AND REPLACED RT SHEAR PANEL AT FR 87 SHEAR PANEL PN170-91919-001. AIRCRAFT REMAINS IN HEAVE CHECK BNA SEE EAMS WO H5339 SEQ1508 SN 102 FOR WORK DETAILS.
CORROSION RT AFT BEAM FR 87. REMOVED AND REPLACED BEAM PART NUMBER 170-65669-004 REF SRM 51-23-04& 51-40-02. AIRCRAFT REMAINS IN HEAVY CHECK.
CORROSION IN CROWN TEETH RT SEAT TRACK FR 82. REMOVED AND REPLACED SEAT TRACK BETWEEN FR 73.5 AN FR 84 AND REINSTALL 15 SEAT TRACK SPLICES 8 TMCLIPS 4 MONUMENTS AND 1 EA BRACKET REF SRM II 51-43-04 51-43-03 51-41 02 RT SEAT TRACK PN REF. WORK ACCOMPLISHED ON WO H5339 SEQ 110. P/N 170-86082-005
REF WORK ACCOMPLISHED ON WO H5339 SEQ1510 SN 104 FOR WORK DETAILS. P/N 170-86082-005
CORROSION IN LT AFT BEAM BETWEEN FR. 87-88 BLENDED CORROSION. PERFORMED HFEC. INSTALLED REPAIR DOUBLER PER SRM 53-23-10 R03. AIRCRAFT REMAINS IN HEAVY CHECK BNA
CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERFORMED A QUICK CHARGE OF THE EMERGENCY LIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD.
CORROSION IN CROWN TEETH LT SEAT TRACK. INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 81-82 TO FR 85 SRM 53-0-10 AND ETD216-170-114510 PN PE11056-F3C. AIRCRAFT REMAINS IN HEAVY CHECK BN.
DURING HEAVY CHECK, RT SPLICE PLATE AT FRAME 87-88 IS CORRODED. MAINTENANCE R & R RT SPLICE PLATE IAW SRM 170 51-41-02.
DURING HEAVY CHECK, LT SPLICE PLATE IS CORRODED. MAINTENANCE REMOVED, LOCATED AND DRILLED NEW SPLICE PLATE, INSTALLED LT SPLICE PLATE IAW SRM 51-42-02, 51-40-02, 51-23-04.
DURING HEAVY CHECK, RT FLOORBEAM AT FRAME 84 IS CORRODED. MAINTENANCE R & R RT FLOORBEAM IAW SRM 51-41-01, 51-41-02, 51-43-04, PN 170-92908-001, FLOOR SILL.
DURING HEAVY CHECK, RT SHEAR PLATE AT FRAME 87-88 IS CORRODED. MAINTENANCE R & R RT SHEAR PLATE AT FRAME 87-88 IAW SRM 51-40-02, 51-23-04, PN 170-66409-001, SHEAR PLATE. ACFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.
DURING HEAVY CHECK, RT FLOORBEAM AT FRAME 18, AT RIVET IS CORRODED. MAINTENANCE REPAIRED DAMAGE TO RT FLOORBEAM AT FRAME 18 IAW ETD 2015-170-102258, SRM 51-10-03, PN 170-03264-001 SEAT TRACK.
DURING HEAVY CHECK, LT SHEAR PLATE AT FRAMES 87-88 IS CORRODED. MAINTENANCE R & R LT SHEAR PLATE IAW SRM 170 51-21-02, AND 51-42-01.
DURING HEAVY CHECK, RT FLOOR SUPPORT AT FRAMES 86-90 IS CORRODED. MAINTENANCE R & R RT FLOOR SUPPORT IAW SRM 51-42-01, 51-43-03.
DURING HEAVY CHECK, RT AFT FLOORBEAM AT FRAME 17 IS CORRODED. MAINTENANCE R & R RT AFT FLOORBEAM IAW SRM 51-41-02, 51-43-04, PN 170-05661-003, SILL.
DURING HEAVY CHECK, WAS REPORTED THAT CENTER SPLICE AT FRAME 90 IS CORRODED. MAINTENANCE R & R CENTER SPLICE AT FRAME 90, PN 170-86119-005, FRAME.
DURING HEAVY CHECK RT SEAT TRACK Y=10.748 AT FRAME 84 IS CORRODED. MAINTENANCE BLENDED AND FABRICATED DOUBLER AND INSTALLED IAW ETD-170-102078.
DURING HEAVY CHECK CENTER SHEAR PLATE FRAME 87-88 IS CORRODED. MAINTENANCE R & R CENTER SHEAR PLATE FRAME 87-88 IAW SRM 51-42-01, 51-21-02, 51-23-05, 51-23-06, PN 170-66408-001, SHEAR PLATE.
MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT AT SEAT 1D WAS LOOSE. MAINTENANCE SECURED THE EMERGENCY LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE AUTO PILOT DISENGAGED AND SHORTLY AFTER RECEIVED SLAT FAIL, SHAKER ANTICIPATED, AP FAIL, AOA LIMIT FAIL AND SPOILER FAIL MESSAGES. CREW RAN QRH, CONTACTED MAINTENANCE CONTROL AND ELECTED TO CONTINUE. ABOUT 100 MILES FROM DESTINATION, CREW DECLARED AN EMERGENCY AND WITH EMERGENCY VEHICLES ROLLING, LANDED WITHOUT INCIDENT. AFTER BEING CHECKED OUT BY FIRE & RESCUE, CREW TAXIED TO GATE WHERE PASSENGERS DEPLANNED NORMALLY. MAINTENANCE TROUBLESHOT, RESET POWER, CLEARED SF ACE INHIBITS IAW AMM AND FAULTS CLEARED. ACFT IS GOOD FOR SERVICE.
CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT HOLDER WAS BROKEN. MAINTENANCE R & R FORWARD F/A FLASHLIGHT HOLDER IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE L2 DOOR WOULD NOT CLOSE. MAINTENANCE INSPECTED IAW AMM AND REMOVED DEBRIS FROM THE L2 DOOR SUPPORT ARM. DOOR OPS CHECKED GOOD AND ACFT IS GOOD FOR SERVICE.
DURING HEAVY CHECK, AFT GALLEY SPLIT JOINTS CORRODED AND NEEDS REPLACED. MAINTENANCE R & R CORRODED SPLIT JOINT BRACKET AND SPLIT JOINT TRIM ON BOTH HALVES ON AFT GALLEY IAW AMM 20-10-01, 25-00-23, PN CDS82200-11, SPLIT JOINT BRACKET. ACFT REMAINS, UNTIL HEAVY CHECK IS COMPLETED.
DURING HEAVY CHECK, RT HORIZONTAL L/E RIB 4 CRACKED AND TOOL DAMAGE ON 2 OTHER RIBS. MANTENANCE CUT OUT DAMAGE AT RIB 4 AND INSTALLED RIB REPAIR ANGLE AND FILLER IAW ETD 2013-170-048576.
DURING HEAVY CHECK, LT PACK DUCT BRACKET CRACKED IN SEVERAL PLACES FWD OF LT PACK ASSY. MAINTENANCE R & R NR 2 PACK DUCT BRACKETS IAW SRM 51-40-01. PN 170-92988-401 BRACKET. ACFT REMAINS FOR COMPLETION.
DURING HEAVY CHECK, AFT PASSENGER DOOR AFT LOWER DOOR STOP NUT CORRODED. MX REMOVED AND REPLACED STOP SCREW AND NUT IAW AMM 52-12-2-3. NAS5509-7 NUT. ACFT REMAINS UNTIL COMPLETION OF HEAVY CHECK.
CREW REPORTED THAT THE L1 DOOR WAS MAKING A LOUD VIBRATION & HUMMING NOISE IN FLIGHT. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MX FOUND THE L1 DOOR DEFLECTOR WORN. MX REMOVED DOOR DEFLECTOR AND PLACED ON CDL IAW AMM. ACFT IS GOOD FOR SERVICE.
CREW REPORTED THAT THE CAPTAINS FLASHLIGHT IS DIM. MX REPLACED FLASHLIGHT BATTERY PACK IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT IS DIM. MX REPLACED F/A FLASHLIGHT BATTERY PACK IAW AMM AND OPS CHECKED GOOD.
CREW REPORTED THAT THE FLIGHT ATTENDANT OXYGEN DEMO MASK WAS IN NEED OF REPAIR OR REPLACEMENT. MAINTENANCE REMOVED AND REPLACED O2 DEMO MASK PER EMB AMM AND OPS CHECKED GOOD.
CREW DISCOVERED AFT FLIGHT ATTENDANTS MASK NEEDED TO BE REPLACED. MAINTENANCE REMOVED AND REPLACED DEMO MASK PER EMB AMM. OPS CHECKED GOOD.
CREW REPORTED SUFFERING A LARGE BIRD STRIKE DURING INITIAL CLIMBOUT FROM EYW. CREW REPORTS SLAT FAIL INDICATION ON EICAS, CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT AT RSW.
CREW REPORTED VIBRATION IN FLIGHT DURING CRUISE. CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PER EMB AMM, AND FOUND A/P ELEVATOR SERVO TO BE THE CAUSE. MAINTENANCE REMOVED AND REPLACED A/P ELEV SERVO PER EMB AMM, OPS CHECK GOOD.
CREW REPORTED R-1 DOOR ARMING LEVER WAS HARD TO OPERATE. MAINTENANCE RE-POSITIONED R-1 DOOR LINING AND PERFORMED OPS CHECKS PER EMB AMM, OPS CHECK GOOD.
WHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT ENGINE PYLON PANEL 429DT HARDWARE. MAINTENANCE REMOVED AND REPLACED THE HARDWARE ON THE RT ENGINE PYLON PANEL 429DT IAW EMB 170/175 AMM 20-10-07. REF: P/N'S PE21114-3C8 BOLT & PE21114-3C6 BOLT.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD CARGO DOOR LATCH ASSY CORRODED. MX REMOVED AND REPLACED FWD CARGO DOOR LOCK CABLE LATCH ASSY IAW EMB 175 AMM 52-31-08, AMD AMM 20-10-02. P/N 170-84599-405. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD HALF AFT GALLEY ENTIRE METAL STRIPS IN BETWEEN MID SECTION, EVIDENCE OF CORROSION FOUND. MX REMOVED AND REPLACED AFT GALLEY METAL TRIM PIECES IAW EMB 175 AMM 25-00-23, REPLACED SPRINGS FOR TRASH DOOR THAT WAS DAMAGED IAW EMB 175 AMM 20-10-01. REPLACED PNL IAW C&D ZODIAC CMM 25-27-62. REPLACED WASTE FLAP ASSY IAW C&D ZODIAC CMM 25-27-62. PN'S 170-88838-401, 458-4-2693, 170-88787-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND AFT CARGO DOOR FWD AND AFT HINGE ARM PIVOT PINS CORRODED. P/N 170-69804-005 MX REMOVED AND REPLACED PINS IAW EMB 175 AMM 52-32-24. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND AFT HALF AFT GALLEY ENTIRE METAL STRIPS IN BETWEEN MID SECTION SHOW EVIDENCE OF CORROSION. MX REMOVED AND REPLACED METAL STRIP ON AFT GALLEY IAW EMB 175 AMM 25-00-23, AND REMOVED CORROSION IAW EMB 175 SRM 51-12-01. P/N 170-59521-001, CDSP2200-11, 170-59523-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND LT ENGINE FIRE EXT DISCHARGER TUBE HAS LIGHT SURFACE CORROSION IN INBOARD FLAP WELL ABOVE AFT PYLON AND INSIDE PNL 522CB. MX REMOVED AND REPLACED LT ENGINE FIRE EXT DISCHARGER TUBE INSIDE PNL 522CB IAW EMB 175 AMM 20-10-03. P/N 170-08084-403. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION ON RIGHT BRACKET AT FRAME 90. MAINTENANCE REMOVED AND REPLACED GUSSET IAW EMB 175 SRM 51-41-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND AFT HALF AFT GALLEY ENTIRE FRONT STRIPS SHOW EVIDENCE OF CORROSION. P/N 170-59522-001 MX REMOVED AND REPLACED AFT GALLEY FRONT STRIPS IAW EMB 175 25-00-23. CLEANED AREA IAW 51-12-00. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND AFT CARGO CUTOUT LOWER SILL CORRODED IN SEVERAL PLACES. MX REMOVED AND REPLACED AFT CARGO LOWER SILL IAW EMB 170/175 SRM 54-40-02, 51-41-01. P/N 170-85251-401. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FORWARD FUSELAGE SEAT TRACK BEAM LT AT FR 19 HAS CORROSION. MX REMOVED AND REPLACED LT FWD FUSELAGE SEAT TRACK IAW EMB 175 SRM 51-40-00, 51-40-02. PN 170-03264-001. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE L1 DOOR DAMPNER CORRODED. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR DAMPNER IAW EMB 175 AMM 52-11-27. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND FWD PAX DOOR EMERGENCY SLIDE FITTING ON BOTTOM OF DOOR, HARDWARE CORRODED. MX REMOVED AND REPLACED FWD PAX DOOR EMERGENCY SLIDE FITTING HARDWARE ON BOTTOM OF DOOR IAW EMB 175 AMM 52-11-40. P/N MS14144-4, NAS6604D11, MS24665-153. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE A/C WAS IN FOR HEAVY CHECK FOUND BRAIDED CONDUIT AND ADEL CLAMPS ON WIRE HARNESS INSIDE INBOARD FLAP WELL HAS SURFACE CORROSION ABOVE AFT PYLON. MX CLEANED BRAIDED CONDUIT AND REPLACED ADEL CLAMP ON BRAIDED HARNESS INSIDE INBOARD FLAP WELL ABOVE AFT PYLON IAW SWPM 20-61-20, AND 20-51-00. PN PE27019RE9. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.
WHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE FORWARD FUSELAGE SEAT TRACK BEAM AT RIGHT FRAME 17 CORRODED. MAINTENANCE REMOVED AND REPLACED RT FORWARD FUSELAGE SEAT TRACK AT FRAME 17 IAW EMB 175 SRM 51-40-02, 51-41-00, 51-43-01, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.
DENT IN FWD FUSELAGE REQUIRES MAJOR REPAIR. MTX C/W MAJOR REPAIR PER EMB ETD 2010-170-09029.
CREW REPORTED SLAT FAIL DURING SLAT EXTENSION WHILE ON FINAL. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT INTO PIT. MAINTENANCE WAS DISPATCHED TO THE A/C TO TROUBLESHOOT. MAINTENANCE FOUND BOTH LT O/B SKEW SENSORS TO BE AT FAULT, AND REMOVED AND REPLACED PER EMB AMM. A/C WAS THEN RELEASED BACK INTO SERVICE.